Collected Data for Tests on NACA 0015 Aerofoil with Chord of Length 0.275m. G.U. Aero Report 9209

Galbraith, R. A. M., Dachun, J., Green, R. B. , Gracey, M.W. and Gilmour, R. (1992) Collected Data for Tests on NACA 0015 Aerofoil with Chord of Length 0.275m. G.U. Aero Report 9209. Technical Report. Department of Aerospace Engineering, University of Glasgow.

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Abstract

Herein is presented the collected data for tests in which a NACA 0015 aerofoil with chord of length 0.275m, was subjected to a variety of displacements in pitch about the quarter-chord location at low Reynolds numbers.

Item Type:Research Reports or Papers (Technical Report)
Status:Published
Glasgow Author(s) Enlighten ID:Gilmour, Mr Ross and Green, Dr Richard and Galbraith, Professor Roderick
Authors: Galbraith, R. A. M., Dachun, J., Green, R. B., Gracey, M.W., and Gilmour, R.
College/School:College of Science and Engineering > School of Engineering > Aerospace Sciences
Publisher:Department of Aerospace Engineering, University of Glasgow
Copyright Holders:Copyright © 1992 Department of Aerospace Engineering, University of Glasgow
Publisher Policy:Reproduced with the permission of the Department

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